Rules and Regulations. Final rule; correction

Agency: Federal Aviation Administration, DOT
Action: Final rule; correction
Citation: FR Doc. 02-19034 · RIN 2120-AA64 · Docket No. 98-ANE-43-AD; Amendment 39-12797; AD 2002-13-09 · 14 CFR 39

Summary

This document makes corrections to Airworthiness Directive (AD) 2002-13-09 applicable to Pratt & Whitney JT8D-200 engines that was published in the Federal Register on July 3, 2002 (67 FR 44527). In the regulatory information, Table part B., Parts Requiring Inspection, one item under Description and one item under Engine Manual are incorrect. This document corrects these items. In all other respects, the original document remains the same. EFFECTIVE DATE: July 3, 2002.

Supplementary Information

A final rule airworthiness directive FR Doc, 02-16535 applicable to Pratt & Whitney JT8D-200 series turbofan engines, was published in the Federal Register on July 3, 2002 (67 FR 44527). The following correction is needed: § 39.13 [Corrected] On page 44528, in the third column, in the regulatory information, Table part B., Parts Requiring Inspection, first column, the last Description “Disk, 4th Stage Turbine—” is corrected to read “Disk, 4th Stage Turbine—All P/N's'. On page 44528, in the third column, in the regulatory information, Table part B., Parts Requiring Inspection, second column, the sixth Engine Manual Section “2-53-16” is corrected to read “72-53-16'. Issued in Burlington, MA, on July 22, 2002. Peter A. White, Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. 02-19034 Filed 7-25-02; 8:45 am]